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CLARK V AIRFOIL (clarkv-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: CLARK V AIRFOIL (clarkv-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.57 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-clarkv-il-1000000-n5.txt
Download as CSV file: xf-clarkv-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: CLARK V AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0637   0.04225   0.03945  -0.0949   1.0000   0.0073
 -15.500  -1.0951   0.03551   0.03249  -0.0999   0.9989   0.0073
 -15.250  -1.0949   0.03201   0.02880  -0.1031   0.9962   0.0074
 -15.000  -1.0873   0.02974   0.02637  -0.1042   0.9938   0.0076
 -14.750  -1.0761   0.02799   0.02447  -0.1043   0.9906   0.0077
 -14.500  -1.0589   0.02645   0.02278  -0.1050   0.9885   0.0079
 -14.250  -1.0386   0.02510   0.02129  -0.1058   0.9871   0.0081
 -14.000  -1.0177   0.02362   0.01968  -0.1067   0.9860   0.0085
 -13.750  -0.9948   0.02238   0.01833  -0.1075   0.9850   0.0088
 -13.500  -0.9771   0.02142   0.01729  -0.1068   0.9819   0.0092
 -13.250  -0.9554   0.02052   0.01629  -0.1068   0.9797   0.0096
 -13.000  -0.9317   0.01968   0.01536  -0.1070   0.9779   0.0100
 -12.750  -0.9069   0.01892   0.01449  -0.1074   0.9764   0.0104
 -12.500  -0.8817   0.01818   0.01366  -0.1077   0.9751   0.0109
 -12.250  -0.8581   0.01752   0.01295  -0.1076   0.9732   0.0117
 -12.000  -0.8362   0.01698   0.01236  -0.1070   0.9702   0.0124
 -11.750  -0.8120   0.01645   0.01177  -0.1068   0.9679   0.0131
 -11.500  -0.7868   0.01595   0.01119  -0.1068   0.9658   0.0138
 -11.250  -0.7606   0.01551   0.01073  -0.1069   0.9640   0.0148
 -11.000  -0.7334   0.01515   0.01035  -0.1071   0.9625   0.0156
 -10.750  -0.7093   0.01482   0.00998  -0.1067   0.9598   0.0164
 -10.500  -0.6848   0.01447   0.00957  -0.1063   0.9568   0.0171
 -10.250  -0.6593   0.01413   0.00916  -0.1061   0.9542   0.0176
 -10.000  -0.6334   0.01375   0.00875  -0.1060   0.9518   0.0184
  -9.750  -0.6059   0.01350   0.00849  -0.1061   0.9498   0.0192
  -9.500  -0.5793   0.01328   0.00824  -0.1060   0.9473   0.0199
  -9.250  -0.5541   0.01302   0.00795  -0.1057   0.9440   0.0206
  -9.000  -0.5282   0.01274   0.00763  -0.1054   0.9406   0.0212
  -8.750  -0.5014   0.01249   0.00731  -0.1054   0.9377   0.0217
  -8.500  -0.4737   0.01226   0.00704  -0.1055   0.9351   0.0222
  -8.250  -0.4474   0.01202   0.00675  -0.1053   0.9317   0.0225
  -8.000  -0.4232   0.01152   0.00620  -0.1048   0.9274   0.0234
  -7.750  -0.3967   0.01122   0.00587  -0.1046   0.9234   0.0241
  -7.500  -0.3693   0.01096   0.00558  -0.1047   0.9199   0.0247
  -7.250  -0.3428   0.01073   0.00532  -0.1045   0.9157   0.0254
  -7.000  -0.3163   0.01049   0.00504  -0.1043   0.9109   0.0260
  -6.750  -0.2890   0.01025   0.00476  -0.1043   0.9064   0.0266
  -6.500  -0.2620   0.01002   0.00448  -0.1042   0.9019   0.0272
  -6.250  -0.2352   0.00979   0.00421  -0.1040   0.8964   0.0276
  -6.000  -0.2079   0.00957   0.00394  -0.1039   0.8911   0.0279
  -5.750  -0.1807   0.00938   0.00371  -0.1038   0.8855   0.0281
  -5.500  -0.1538   0.00914   0.00342  -0.1037   0.8793   0.0287
  -5.250  -0.1269   0.00889   0.00311  -0.1035   0.8734   0.0295
  -5.000  -0.0999   0.00868   0.00287  -0.1034   0.8666   0.0303
  -4.750  -0.0725   0.00851   0.00265  -0.1033   0.8602   0.0310
  -4.500  -0.0453   0.00835   0.00248  -0.1031   0.8532   0.0319
  -4.000   0.0094   0.00810   0.00215  -0.1029   0.8391   0.0337
  -3.500   0.0642   0.00790   0.00188  -0.1027   0.8246   0.0358
  -3.250   0.0913   0.00779   0.00175  -0.1026   0.8173   0.0398
  -3.000   0.1187   0.00768   0.00165  -0.1025   0.8097   0.0443
  -2.500   0.1729   0.00747   0.00148  -0.1022   0.7943   0.0665
  -2.250   0.1998   0.00739   0.00140  -0.1020   0.7863   0.0767
  -2.000   0.2270   0.00731   0.00133  -0.1019   0.7775   0.0865
  -1.750   0.2536   0.00724   0.00127  -0.1016   0.7667   0.1034
  -1.500   0.2793   0.00714   0.00123  -0.1012   0.7521   0.1334
  -1.250   0.3049   0.00709   0.00118  -0.1007   0.7347   0.1597
  -1.000   0.3303   0.00700   0.00115  -0.1003   0.7189   0.1970
  -0.750   0.3556   0.00683   0.00113  -0.0999   0.7059   0.2614
  -0.500   0.3811   0.00670   0.00113  -0.0995   0.6936   0.3226
  -0.250   0.4067   0.00660   0.00114  -0.0991   0.6805   0.3733
   0.000   0.4326   0.00653   0.00116  -0.0988   0.6675   0.4197
   0.250   0.4583   0.00649   0.00118  -0.0984   0.6535   0.4612
   0.500   0.4834   0.00650   0.00122  -0.0979   0.6360   0.4992
   0.750   0.5077   0.00647   0.00127  -0.0972   0.6158   0.5559
   1.000   0.5311   0.00636   0.00135  -0.0964   0.5947   0.6478
   1.250   0.5526   0.00620   0.00145  -0.0951   0.5732   0.7631
   1.500   0.5747   0.00614   0.00156  -0.0938   0.5536   0.8428
   1.750   0.5975   0.00615   0.00167  -0.0925   0.5373   0.9006
   2.000   0.6232   0.00625   0.00178  -0.0919   0.5220   0.9436
   2.250   0.6545   0.00641   0.00189  -0.0927   0.5048   0.9655
   2.500   0.6859   0.00660   0.00199  -0.0936   0.4844   0.9772
   2.750   0.7165   0.00683   0.00211  -0.0943   0.4600   0.9858
   3.000   0.7474   0.00708   0.00225  -0.0952   0.4343   0.9927
   3.500   0.8059   0.00767   0.00256  -0.0963   0.3749   1.0000
   3.750   0.8250   0.00798   0.00272  -0.0946   0.3445   1.0000
   4.000   0.8458   0.00824   0.00288  -0.0933   0.3220   1.0000
   4.250   0.8678   0.00848   0.00304  -0.0922   0.3039   1.0000
   4.500   0.8904   0.00870   0.00320  -0.0912   0.2888   1.0000
   4.750   0.9128   0.00895   0.00337  -0.0902   0.2708   1.0000
   5.000   0.9352   0.00922   0.00356  -0.0892   0.2527   1.0000
   5.250   0.9580   0.00948   0.00375  -0.0883   0.2373   1.0000
   5.500   0.9809   0.00973   0.00394  -0.0875   0.2231   1.0000
   5.750   1.0030   0.01004   0.00417  -0.0865   0.2053   1.0000
   6.000   1.0241   0.01041   0.00444  -0.0854   0.1833   1.0000
   6.250   1.0459   0.01074   0.00469  -0.0843   0.1678   1.0000
   6.500   1.0678   0.01106   0.00495  -0.0834   0.1543   1.0000
   6.750   1.0890   0.01142   0.00523  -0.0823   0.1388   1.0000
   7.000   1.1094   0.01181   0.00554  -0.0811   0.1221   1.0000
   7.250   1.1284   0.01224   0.00587  -0.0795   0.1037   1.0000
   7.500   1.1465   0.01271   0.00624  -0.0779   0.0871   1.0000
   7.750   1.1656   0.01311   0.00660  -0.0765   0.0763   1.0000
   8.000   1.1845   0.01354   0.00699  -0.0750   0.0661   1.0000
   8.250   1.2024   0.01403   0.00741  -0.0734   0.0540   1.0000
   8.500   1.2188   0.01462   0.00791  -0.0716   0.0404   1.0000
   8.750   1.2346   0.01524   0.00846  -0.0697   0.0281   1.0000
   9.000   1.2504   0.01588   0.00904  -0.0679   0.0194   1.0000
   9.250   1.2675   0.01642   0.00959  -0.0662   0.0157   1.0000
   9.500   1.2857   0.01690   0.01008  -0.0648   0.0140   1.0000
   9.750   1.3029   0.01743   0.01063  -0.0633   0.0126   1.0000
  10.000   1.3198   0.01798   0.01121  -0.0618   0.0115   1.0000
  10.250   1.3375   0.01849   0.01175  -0.0604   0.0109   1.0000
  10.500   1.3543   0.01905   0.01235  -0.0589   0.0103   1.0000
  10.750   1.3702   0.01966   0.01299  -0.0573   0.0097   1.0000
  11.000   1.3853   0.02034   0.01370  -0.0557   0.0091   1.0000
  11.250   1.3997   0.02106   0.01446  -0.0540   0.0086   1.0000
  11.500   1.4152   0.02172   0.01517  -0.0525   0.0082   1.0000
  11.750   1.4297   0.02243   0.01593  -0.0510   0.0079   1.0000
  12.000   1.4436   0.02321   0.01676  -0.0494   0.0075   1.0000
  12.250   1.4568   0.02404   0.01764  -0.0478   0.0072   1.0000
  12.500   1.4688   0.02496   0.01860  -0.0461   0.0069   1.0000
  12.750   1.4798   0.02598   0.01967  -0.0444   0.0067   1.0000
  13.000   1.4888   0.02717   0.02092  -0.0425   0.0064   1.0000
  13.250   1.4998   0.02822   0.02204  -0.0410   0.0062   1.0000
  13.500   1.5100   0.02935   0.02324  -0.0394   0.0061   1.0000
  13.750   1.5194   0.03057   0.02454  -0.0379   0.0060   1.0000
  14.000   1.5280   0.03190   0.02594  -0.0365   0.0058   1.0000
  14.250   1.5358   0.03330   0.02741  -0.0350   0.0056   1.0000
  14.500   1.5428   0.03482   0.02900  -0.0336   0.0055   1.0000
  14.750   1.5491   0.03643   0.03068  -0.0323   0.0053   1.0000
  15.000   1.5546   0.03818   0.03250  -0.0311   0.0052   1.0000
  15.250   1.5591   0.04007   0.03447  -0.0300   0.0051   1.0000
  15.500   1.5624   0.04214   0.03661  -0.0290   0.0049   1.0000
  15.750   1.5638   0.04450   0.03904  -0.0280   0.0048   1.0000
  16.000   1.5630   0.04718   0.04183  -0.0272   0.0047   1.0000
  16.250   1.5605   0.05014   0.04490  -0.0266   0.0046   1.0000
  16.500   1.5603   0.05294   0.04780  -0.0262   0.0045   1.0000
  16.750   1.5592   0.05597   0.05092  -0.0260   0.0045   1.0000
  17.000   1.5564   0.05930   0.05436  -0.0261   0.0044   1.0000
  17.250   1.5527   0.06284   0.05801  -0.0263   0.0044   1.0000
  17.500   1.5469   0.06676   0.06203  -0.0267   0.0043   1.0000
  17.750   1.5402   0.07091   0.06630  -0.0274   0.0043   1.0000
  18.000   1.5316   0.07547   0.07098  -0.0284   0.0042   1.0000
  18.250   1.5216   0.08036   0.07598  -0.0296   0.0042   1.0000
  18.500   1.5097   0.08561   0.08136  -0.0311   0.0042   1.0000
  18.750   1.4959   0.09130   0.08718  -0.0329   0.0041   1.0000
  19.000   1.4809   0.09736   0.09336  -0.0350   0.0041   1.0000
  19.250   1.4647   0.10373   0.09986  -0.0374   0.0041   1.0000
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